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链翼无人机续航性能及气动特性研究

周伟 韩世龙 马培洋 王金金 王凯

航空科学技术2025,Vol.36Issue(12):1-9,9.
航空科学技术2025,Vol.36Issue(12):1-9,9.DOI:10.19452/j.issn1007-5453.2025.12.001

链翼无人机续航性能及气动特性研究

Research on Endurance Performance and Aerodynamic Characteristics of Chained-Wing UAVs

周伟 1韩世龙 1马培洋 1王金金 1王凯1

作者信息

  • 1. 火箭军工程大学,陕西西安 710025
  • 折叠

摘要

Abstract

The chained-wing technology based on wingtip docking can significantly improve the aerodynamic performance and endurance of traditional UAV swarms.This paper focused on chained-wing UAVs,employed the vortex lattice method to calculate aerodynamic characteristics of various geometric configurations.A comprehensive investigation was conducted on configuration effects,and an endurance performance model was developed to study wingtip connection impacts.Research results revealed that wingtip connection could significantly reduce induced drag.In 8-unit configuration,the maximum lift-drag ratio increased to 56.3 with 47%reduction in average cruise power,while endurance time and range improved by 94%and 92%respectively.Considering practical mission requirements and system reliability,the optimal number of chain-wing units should not exceed 8.Considering practical mission requirements and system reliability,the number of chained-wing units should not exceed eight.Configuration changes had minimal effects on the aerodynamic performance of the system;for example,when a relative roll angle of 20° occurred in a two-unit chained-wing UAVs,the lift coefficient decreased by a maximum of 5%,while the drag coefficient decreased by 2%.Increasing the dihedral and sweep angles of the wings reduced the lift coefficient of the system,indicating that rectangular straight wings are more suitable for the wing design of chained-wing UAVs.This study provide theoretical foundation for the design optimization and performance evaluation of chained-wing UAVs.

关键词

链翼无人机/无人机集群/涡格法/续航性能/气动特性

Key words

chained-wing UAVs/UAV swarms/vortex lattice method/endurance performance/aerodynamic characteristics

分类

航空航天

引用本文复制引用

周伟,韩世龙,马培洋,王金金,王凯..链翼无人机续航性能及气动特性研究[J].航空科学技术,2025,36(12):1-9,9.

基金项目

航空科学基金(201829U8007) Aeronautical Science Foundation of China(201829U8007) (201829U8007)

航空科学技术

1007-5453

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